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斜劈式翼型扰流柱冷却通道流动与换热数值研究
引用本文:贾宁,靳伟,武俊梅. 斜劈式翼型扰流柱冷却通道流动与换热数值研究[J]. 航空动力学报, 2021, 36(1): 61-69. DOI: 10.13224/j.cnki.jasp.2021.01.008
作者姓名:贾宁  靳伟  武俊梅
作者单位:西安交通大学航天航空学院机械结构强度与振动国家重点实验室,西安710049;西安交通大学能源与动力工程学院热流科学与工程教育部重点实验室,西安710049
基金项目:国家科技重大专项(2017-Ⅲ-0003-0027)
摘    要:基于NACA翼型和斜劈式纵向涡发生器结构设计了一种新型斜劈式翼型扰流柱及其在冷却通道内的排布形式,采用数值模拟方法对含有该种翼型扰流柱的涡轮叶片冷却通道流动换热特性进行了研究,得到了流场和温度场的详细特征及含有斜劈式翼型扰流柱冷却通道的换热能力。分析结果表明:斜劈式翼型扰流柱有良好的强化换热效果。该翼型扰流柱的斜劈式结构可以在其尾缘后方形成持久而稳定的二次流纵向涡,有助于加强流场的扰动作用,从而增强通道换热能力。 

关 键 词:扰流柱  翼型  迎角  斜劈  流动换热特性  尾缘冷却
收稿时间:2020-06-16

Numerical investigation on flow and heat transfer of beveled pin-fins based on airfoil profile in a cooling channel
JIA Ning,JIN Wei,WU Junmei. Numerical investigation on flow and heat transfer of beveled pin-fins based on airfoil profile in a cooling channel[J]. Journal of Aerospace Power, 2021, 36(1): 61-69. DOI: 10.13224/j.cnki.jasp.2021.01.008
Authors:JIA Ning  JIN Wei  WU Junmei
Affiliation:State Key Laboratory for Strength and Vibration of Mechanical Structures,School of Aerospace Engineering,Xi’an Jiaotong University,Xi’an 710049,China
Abstract:Based on NACA airfoil profile and the structure of beveled vortice generator, a novel beveled design of NACA pin-fin and its configuration in the cooling channel of turbine blade were proposed. Numerical simulation was conducted to investigate the flow and heat transfer characteristics of this pin-fin arrays in the cooling channel. The detailed physical field distributions of the flow and heat transfer were discussed and the overall thermal performance was also explored. The result indicated that the bevel cut of the pin-fin can produce lasting and stable longitudinal vortices to strengthen the disturbance of flow field, yielding a good effect on enhancing heat transfer of the cooling channel.
Keywords:pin-fin  airfoil profile  attack angle  bevel cut  ,flow and heat transfer performance  trailing edge cooling
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